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MACH TRIM Switch/Light
(momentary-action)
INOP Light
Press - Alternately engages or
disengages the Mach trim function
Illuminated - Indicates Mach trim
function is inoperative/disengaged
STAB TRIM CH1, CH2 Switches
(momentary-action)
Press - Engages respective
channel of the Horizontal Stabilizer
Trim Control Unit (HSTCU)
I/C
OFF
R/T
NOSE
DN
NOSE
UP
AP
SC
SYNC
FLIGHT CONTROLS
10-26 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Flaps, Spoilers
Flap and Spoiler Controls
Figure 10-15
0
20
30
45
0
20
30
45
FLAPS
GND SPOILERS
ARM
AUTO
DISARM
FLIGHT
SPOILER
1/4
0
RETRACT
1/2
3/4
MAX
FLIGHT SPOILER
LEVER
FLAP SELECTOR LEVER
FLAP Selector
Lever
Sets flap position
0° - Taxiing, flight
20° - Takeoff
30° - Approach
45° - Landing
THRUST REVERSER/
SPOILER CONTROL PANEL
P604_10_011
GND SPOILERS Switch
ARM
AUTO
DISARM
- Manually arms the ground spoilers
for deployment
- Arms the ground spoilers for
automatic deployment
- Disarms the ground spoilers in
the event of an inadvertent deployment or
failure of automatic system
FLIGHT SPOILER Lever
- Positions flight spoilers to
selected detent
- 0, 1/4, 1/2, 3/4, MAX detents
: Four additional
detented positions are possible
between the above indicated
positions.
NOTE
FLIGHT CONTROLS
For Training Purposes Only
May 03
10-27
P I LOT T R A I N I N G GU I D E
Stall Protection System
Stall Protection System
Figure 10-16
TEST
TEST
TEST
TEST
TEST
WARN
TEST
FIRE DET
1 2 APU
BOTTLE
FAIL
L R G SWITCH
SPS TEST
FIREX MONITOR AURAL
WARN TEST
LAMP
TEST
OVSP
TEST
1
2
1
2
1
2
ENG BOTTLE
STALL
PROT
PUSHER
ON
OFF
SPS TEST
INDICATOR
STALL
PROT
PUSHER
ON
OFF
SPS TEST
INDICATOR
LH ENG
FIRE
PUSH
GPWS
TERR
INHB
MASTER
WARNING BOTTLE 1
ARMED
PUSH TO
DISCH
STALL
MASTER
CAUTION
PULL UP
GND PROX
ATS
N2 SYNC
ATS
N1 TO
FAIL
ATS
N1 TO
FAIL
APU
FIRE
PUSH
RH ENG
FIRE
PUSH
GPWS
TERR
INHB
MASTER
BOTTLE 2 WARNING
ARMED
PUSH TO
DISCH
BOTTLE
ARMED
PUSH TO
DISCH
STALL
MASTER
CAUTION
PULL UP
GND PROX
STALL PROT PUSHER Switch
ON - Stick pusher is armed
OFF - Stick pusher is disabled
NOTE: Both pilot's and copilot's
PUSHER switches must be ON to
arm the stick pusher.
SPS TEST Indicator
Blue Sector - Continuous ignition is activated
Yellow Sector - Stick shaker operates
Red Sector - Aural stall warning and stick pusher
operates
STALL PROTECTION PANEL
(PILOT'S SIDE)
STALL PROTECTION PANEL
(COPILOT'S SIDE)
I/C
OFF
R/T
NOSE
DN
NOSE
UP
AP
SC
SYNC
PILOT’S SIDE
COPILOT’S SIDE
STALL Lights
Illuminated Flashing - Indicate AOA has reached
stick pusher trip point (during flight or an SPS test)
COPILOT’S CONTROL WHEEL
(MIRROR OF PILOT’S)
AP/SP (Autopilot/Stick
Pusher Disconnect) Button
Press - Disengages autopilot
and deactivates stick pusher
NOTE: When released, stick
pusher system is immediately
reactivated.
P604_10_012
L and R SPS TEST Switches
(spring-loaded off)
TEST - Tests respective
channel of Stall Protection
System (SPS) Computer
SPS TEST G Switch
(spring-loaded off)
TEST - Deactivates
stick pusher during SPS
preflight test
MISCELLANEOUS TEST PANEL
FLIGHT CONTROLS
10-28 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
EICAS Flight Controls Indications (Ground Spoilers)
Figure 10-17
P604_10_019
FLIGHT CONTROLS
AIL AIL
FLAPS 30
Description Symbol Condition
Ground spoilers are fully extended
Note: Indicators are not displayed when ground
spoilers are retracted or input data is invalid.
Ground Spoiler Position
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庞巴迪挑战者604机组操作手册 CL_604-FLIGHT_CONTROLS(10)
